Date:
June 7th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4843 76 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2007/157/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 432139
17 A = 6708539
75 meter
Y = 4233989
25 meter E =
0006613
Z = -5191261
64 I = 51
73074
XDOT = -7357
230087 Wp = 87
32530
YDOT = 2029
863040 meter/sec RA = 158
37757 deg
ZDOT = 1044
551913 TA = 192
61203
MA = 192
62859
Ha = 182
387 n
mi
Hp = 180
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1417779
41 X = 409980
05
Y = 13891040
85 feet Y = 4238698
58 meter
Z = -17031698
31 Z = -5189215
49
XDOT = -24137
893985 XDOT = -7384
455727
YDOT = 6659
655644 feet/sec YDOT = 1947
437980 meter/sec
ZDOT = 3427
007587 ZDOT = 1008
744834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12660037
27 X = 3858779
36
Y = 5913996
97 feet Y = 1802586
28 meter
Z = -17023453
17 Z = -5188748
53
XDOT = -6409
281778 XDOT = -1953
549086
YDOT = 23182
887811 feet/sec YDOT = 7066
144205 meter/sec
ZDOT = 3292
058392 ZDOT = 1003
419398
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07157
47248306
00020000 00000-0 20000-3 0 9003
2 25544 51
6324 159
2842 0008160 286
4738 73
5530 15
78180870 9082
Satellite: ISS
Catalog Number: 25544
Epoch time: 07157
47248306 = yrday
fracday
Element set: 900
Inclination: 51
6324 deg
RA of node: 159
2842 deg
Eccentricity:
0008160
Arg of perigee: 286
4738 deg
Mean anomaly: 73
5530 deg
Mean motion: 15
78180870 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 908
Checksum: 297
Coasting Arc #2 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2007/158/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6220507
89 A = 6718062
69 meter
Y = -1144665
40 meter E =
0003830
Z = -2258491
44 I = 51
78839
XDOT = -1007
376731 Wp = 245
02171
YDOT = 5331
165003 meter/sec RA = 153
24698 deg
ZDOT = -5470
972519 TA = 320
31802
MA = 320
34604
Ha = 182
499 n
mi
Hp = 180
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20408490
44 X = 6243816
69
Y = -3755463
93 feet Y = -1074973
57 meter
Z = -7409748
83 Z = -2228215
83
XDOT = -3305
041770 XDOT = -1040
338811
YDOT = 17490
698828 feet/sec YDOT = 5319
716376 meter/sec
ZDOT = -17949
384906 ZDOT = -5475
945700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7064516
25 X = 2153264
55
Y = -19554582
15 feet Y = -5960236
64 meter
Z = -7295566
88 Z = -2223688
79
XDOT = 12064
863645 XDOT = 3677
370439
YDOT = 11069
106448 feet/sec YDOT = 3373
863645 meter/sec
ZDOT = -17967
508219 ZDOT = -5476
496505
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07158
48560385
00020000 00000-0 20000-3 0 9010
2 25544 51
6314 154
0477 0008082 290
4092 69
6205 15
78210037 9241
Satellite: ISS
Catalog Number: 25544
Epoch time: 07158
48560385 = yrday
fracday
Element set: 901
Inclination: 51
6314 deg
RA of node: 154
0477 deg
Eccentricity:
0008082
Arg of perigee: 290
4092 deg
Mean anomaly: 69
6205 deg
Mean motion: 15
78210037 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 924
Checksum: 283
Coasting Arc #3 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2007/159/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2066441
22 A = 6713061
63 meter
Y = -4989324
72 meter E =
0006577
Z = 3989128
57 I = 51
79692
XDOT = 6594
672340 Wp = 29
66477
YDOT = -441
090594 meter/sec RA = 148
04356 deg
ZDOT = -3959
479317 TA = 101
21400
MA = 101
14007
Ha = 182
663 n
mi
Hp = 179
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6779662
79 X = 2102700
51
Y = -16369175
60 feet Y = -4966014
35 meter
Z = 13087692
17 Z = 3999254
84
XDOT = 21636
064107 XDOT = 6618
349001
YDOT = -1447
147619 feet/sec YDOT = -367
212421 meter/sec
ZDOT = -12990
417707 ZDOT = -3927
384904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10997031
46 X = -3351895
19
Y = -13856144
30 feet Y = -4223352
78 meter
Z = 13125318
57 Z = 4000597
10
XDOT = 8345
753063 XDOT = 2543
785533
YDOT = -18840
093905 feet/sec YDOT = -5742
460622 meter/sec
ZDOT = -12869
272911 ZDOT = -3922
554383
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07159
49870731
00020000 00000-0 20000-3 0 9022
2 25544 51
6309 148
8110 0008189 295
2069 64
8247 15
78270662 9406
Satellite: ISS
Catalog Number: 25544
Epoch time: 07159
49870731 = yrday
fracday
Element set: 902
Inclination: 51
6309 deg
RA of node: 148
8110 deg
Eccentricity:
0008189
Arg of perigee: 295
2069 deg
Mean anomaly: 64
8247 deg
Mean motion: 15
78270662 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 940
Checksum: 310
Coasting Arc #4 (Orbit 955)
---------------------------------------
Vector Time (GMT): 2007/160/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5045242
90 A = 6711716
55 meter
Y = -520077
84 meter E =
0001831
Z = 4393854
68 I = 51
81522
XDOT = 3534
998164 Wp = 66
85860
YDOT = -5973
313015 meter/sec RA = 142
93711 deg
ZDOT = 3351
640044 TA = 349
55175
MA = 349
55556
Ha = 182
975 n
mi
Hp = 179
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16552634
18 X = -5060397
02
Y = -1706292
12 feet Y = -576581
81 meter
Z = 14415533
74 Z = 4369307
87
XDOT = 11597
763006 XDOT = 3585
248135
YDOT = -19597
483645 feet/sec YDOT = -5933
502105 meter/sec
ZDOT = 10996
194369 ZDOT = 3368
934543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9387454
73 X = -2861296
20
Y = 13836284
16 feet Y = 4217299
41 meter
Z = 14322767
83 Z = 4365579
64
XDOT = -10777
708412 XDOT = -3285
045524
YDOT = -18763
322261 feet/sec YDOT = -5719
060625 meter/sec
ZDOT = 11060
775759 ZDOT = 3371
324451
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07160
51179571
00020000 00000-0 20000-3 0 9032
2 25544 51
6302 143
5742 0008227 299
1412 60
8929 15
78271445 9560
Satellite: ISS
Catalog Number: 25544
Epoch time: 07160
51179571 = yrday
fracday
Element set: 903
Inclination: 51
6302 deg
RA of node: 143
5742 deg
Eccentricity:
0008227
Arg of perigee: 299
1412 deg
Mean anomaly: 60
8929 deg
Mean motion: 15
78271445 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 956
Checksum: 294
Coasting Arc #5 (Orbit 970)
---------------------------------------
Vector Time (GMT): 2007/161/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3864670
71 A = 6718722
15 meter
Y = 5239672
95 meter E =
0010817
Z = -1629307
20 I = 51
86159
XDOT = -4806
581367 Wp = 349
71053
YDOT = -1752
830697 meter/sec RA = 137
74354 deg
ZDOT = 5768
756282 TA = 352
31135
MA = 352
32792
Ha = 182
935 n
mi
Hp = 179
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12679365
86 X = -3915059
30
Y = 17190528
04 feet Y = 5196174
50 meter
Z = -5345496
07 Z = -1648203
71
XDOT = -15769
623906 XDOT = -4814
647601
YDOT = -5750
756880 feet/sec YDOT = -1806
626420 meter/sec
ZDOT = 18926
365756 ZDOT = 5745
385834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9470036
28 X = 2886467
06
Y = 19126886
90 feet Y = 5829875
13 meter
Z = -5416226
68 Z = -1650865
89
XDOT = -10999
194991 XDOT = -3352
554633
YDOT = 10776
061884 feet/sec YDOT = 3284
543662 meter/sec
ZDOT = 18837
887960 ZDOT = 5741
788250
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07161
46154998
00020000 00000-0 20000-3 0 9044
2 25544 51
6300 138
6652 0008064 302
8946 57
1443 15
78318419 9716
Satellite: ISS
Catalog Number: 25544
Epoch time: 07161
46154998 = yrday
fracday
Element set: 904
Inclination: 51
6300 deg
RA of node: 138
6652 deg
Eccentricity:
0008064
Arg of perigee: 302
8946 deg
Mean anomaly: 57
1443 deg
Mean motion: 15
78318419 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 971
Checksum: 302
Coasting Arc #6 (Orbit 986)
---------------------------------------
Vector Time (GMT): 2007/162/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3229328
76 A = 6707867
30 meter
Y = 2611134
89 meter E =
0010088
Z = -5275146
18 I = 51
84463
XDOT = -5073
912860 Wp = 57
29689
YDOT = 5789
615548 meter/sec RA = 132
60694 deg
ZDOT = -235
331805 TA = 210
44688
MA = 210
50550
Ha = 183
249 n
mi
Hp = 179
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10594910
64 X = 3225516
73
Y = 8566715
52 feet Y = 2647226
55 meter
Z = -17306910
04 Z = -5259466
74
XDOT = -16646
695736 XDOT = -5137
132866
YDOT = 18994
801666 feet/sec YDOT = 5732
522763 meter/sec
ZDOT = -772
085974 ZDOT = -260
133915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12419820
73 X = 3785561
36
Y = -5783251
43 feet Y = -1762735
04 meter
Z = -17247374
80 Z = -5256999
84
XDOT = 9222
242000 XDOT = 2810
939361
YDOT = 22434
356220 feet/sec YDOT = 6837
991776 meter/sec
ZDOT = -865
068537 ZDOT = -263
672890
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07162
47460507
00020000 00000-0 20000-3 0 9053
2 25544 51
6294 133
4275 0008230 307
0012 53
0399 15
78310086 9872
Satellite: ISS
Catalog Number: 25544
Epoch time: 07162
47460507 = yrday
fracday
Element set: 905
Inclination: 51
6294 deg
RA of node: 133
4275 deg
Eccentricity:
0008230
Arg of perigee: 307
0012 deg
Mean anomaly: 53
0399 deg
Mean motion: 15
78310086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 987
Checksum: 277
Coasting Arc #7 (Orbit 1002)
---------------------------------------
Vector Time (GMT): 2007/163/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4747264
00 A = 6719153
08 meter
Y = -4586558
52 meter E =
0001924
Z = -1247681
62 I = 51
90194
XDOT = 2560
220541 Wp = 199
77656
YDOT = 4252
721636 meter/sec RA = 127
46401 deg
ZDOT = -5891
127400 TA = 353
87433
MA = 353
87669
Ha = 183
337 n
mi
Hp = 179
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15575013
14 X = 4804259
85
Y = -15047764
17 feet Y = -4533153
04 meter
Z = -4093443
63 Z = -1224481
46
XDOT = 8399
673690 XDOT = 2541
094164
YDOT = 13952
498805 feet/sec YDOT = 4281
245602 meter/sec
ZDOT = -19327
845802 ZDOT = -5878
735334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6923811
45 X = -2110377
73
Y = -20537344
13 feet Y = -6259782
49 meter
Z = -4006351
51 Z = -1221135
94
XDOT = 14753
698749 XDOT = 4496
927379
YDOT = -1212
220977 feet/sec YDOT = -369
484954 meter/sec
ZDOT = -19280
533054 ZDOT = -5876
706475
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07163
48764257
00020000 00000-0 20000-3 0 9065
2 25544 51
6296 128
1900 0008316 311
5631 48
4821 15
78357163 10037
Satellite: ISS
Catalog Number: 25544
Epoch time: 07163
48764257 = yrday
fracday
Element set: 906
Inclination: 51
6296 deg
RA of node: 128
1900 deg
Eccentricity:
0008316
Arg of perigee: 311
5631 deg
Mean anomaly: 48
4821 deg
Mean motion: 15
78357163 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1003
Checksum: 284
Coasting Arc #8 (Orbit 1018)
---------------------------------------
Vector Time (GMT): 2007/164/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1269283
37 A = 6710563
15 meter
Y = -4731493
29 meter E =
0009644
Z = 4589447
04 I = 51
88963
XDOT = 5563
682358 Wp = 9
77934
YDOT = -4408
145024 meter/sec RA = 122
27873 deg
ZDOT = -2995
633588 TA = 109
88675
MA = 109
78280
Ha = 183
479 n
mi
Hp = 178
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4164315
52 X = -1238575
76
Y = -15523271
96 feet Y = -4745516
42 meter
Z = 15057240
95 Z = 4583354
36
XDOT = 18253
551043 XDOT = 5627
113800
YDOT = -14462
418059 feet/sec YDOT = -4345
573504 meter/sec
ZDOT = -9828
194187 ZDOT = -2968
451742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15893844
31 X = -4844443
75
Y = -2531484
11 feet Y = -771596
36 meter
Z = 15033672
29 Z = 4582263
31
XDOT = -5809
550333 XDOT = -1770
750942
YDOT = -21484
135859 feet/sec YDOT = -6548
364610 meter/sec
ZDOT = -9726
021655 ZDOT = -2964
491400
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07164
50066247
00020000 00000-0 20000-3 0 9074
2 25544 51
6295 122
9528 0008445 314
7820 45
2657 15
78382283 10192
Satellite: ISS
Catalog Number: 25544
Epoch time: 07164
50066247 = yrday
fracday
Element set: 907
Inclination: 51
6295 deg
RA of node: 122
9528 deg
Eccentricity:
0008445
Arg of perigee: 314
7820 deg
Mean anomaly: 45
2657 deg
Mean motion: 15
78382283 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1019
Checksum: 298
Coasting Arc #9 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2007/165/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4773996
58 A = 6713420
12 meter
Y = 2822195
57 meter E =
0007578
Z = 3774415
29 I = 51
91502
XDOT = -440
901890 Wp = 51
14613
YDOT = -6423
163129 meter/sec RA = 117
17715 deg
ZDOT = 4244
046160 TA = 354
48350
MA = 354
49185
Ha = 183
611 n
mi
Hp = 178
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15662718
45 X = -4823535
53
Y = 9259171
81 feet Y = 2768532
19 meter
Z = 12383252
26 Z = 3751103
37
XDOT = -1446
528510 XDOT = -389
661325
YDOT = -21073
369846 feet/sec YDOT = -6427
808039 meter/sec
ZDOT = 13924
035958 ZDOT = 4242
027196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2259243
61 X = 688617
45
Y = 18113930
38 feet Y = 5521125
98 meter
Z = 12295498
89 Z = 3747668
06
XDOT = -18628
364148 XDOT = -5677
925392
YDOT = -7124
605227 feet/sec YDOT = -2171
579673 meter/sec
ZDOT = 13915
668135 ZDOT = 4241
495647
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07165
51366386
00020000 00000-0 20000-3 0 9084
2 25544 51
6304 117
7160 0008406 317
6683 42
3833 15
78442746 10356
Satellite: ISS
Catalog Number: 25544
Epoch time: 07165
51366386 = yrday
fracday
Element set: 908
Inclination: 51
6304 deg
RA of node: 117
7160 deg
Eccentricity:
0008406
Arg of perigee: 317
6683 deg
Mean anomaly: 42
3833 deg
Mean motion: 15
78442746 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1035
Checksum: 292
Coasting Arc #10 (Orbit 1049)
---------------------------------------
Vector Time (GMT): 2007/166/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -391350
01 A = 6716875
35 meter
Y = 6212655
26 meter E =
0010203
Z = -2506198
15 I = 51
93883
XDOT = -5249
448412 Wp = 353
99620
YDOT = 1822
579549 meter/sec RA = 111
97984 deg
ZDOT = 5345
728476 TA = 337
68748
MA = 337
73184
Ha = 183
791 n
mi
Hp = 178
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1283956
72 X = -448617
08
Y = 20382727
22 feet Y = 6207959
37 meter
Z = -8222434
86 Z = -2508236
92
XDOT = -17222
599776 XDOT = -5295
407201
YDOT = 5979
591695 feet/sec YDOT = 1763
619012 meter/sec
ZDOT = 17538
479253 ZDOT = 5320
115444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18375454
05 X = 5600838
40
Y = 8906835
34 feet Y = 2714803
41 meter
Z = -8229430
21 Z = -2508330
33
XDOT = -417
490669 XDOT = -127
251156
YDOT = 16952
479855 feet/sec YDOT = 5167
115860 meter/sec
ZDOT = 17441
901367 ZDOT = 5316
291537
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07166
46333911
00020000 00000-0 20000-3 0 9098
2 25544 51
6307 112
8060 0008459 322
7892 37
2686 15
78418576 10501
Satellite: ISS
Catalog Number: 25544
Epoch time: 07166
46333911 = yrday
fracday
Element set: 909
Inclination: 51
6307 deg
RA of node: 112
8060 deg
Eccentricity:
0008459
Arg of perigee: 322
7892 deg
Mean anomaly: 37
2686 deg
Mean motion: 15
78418576 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1050
Checksum: 301
Coasting Arc #11 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2007/167/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284009
22 A = 6707977
87 meter
Y = -172279
08 meter E =
0013262
Z = -5168575
90 I = 51
91967
XDOT = -1235
016450 Wp = 44
48281
YDOT = 7494
142975 meter/sec RA = 106
86339 deg
ZDOT = -1266
131533 TA = 213
41762
MA = 213
50139
Ha = 183
907 n
mi
Hp = 178
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055148
35 X = 4310725
12
Y = -565220
06 feet Y = -124222
29 meter
Z = -16957270
02 Z = -5147699
45
XDOT = -4051
891240 XDOT = -1312
574663
YDOT = 24587
083251 feet/sec YDOT = 7479
898976 meter/sec
ZDOT = -4153
974845 ZDOT = -1272
317838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4636458
09 X = 1413192
43
Y = -13380538
75 feet Y = -4078388
21 meter
Z = -16878391
94 Z = -5144533
86
XDOT = 20446
539662 XDOT = 6232
105289
YDOT = 12383
594778 feet/sec YDOT = 3774
519688 meter/sec
ZDOT = -4176
504126 ZDOT = -1272
998458
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07167
47630739
00020000 00000-0 20000-3 0 9100
2 25544 51
6317 107
5686 0008513 326
1323 33
9298 15
78454183 10668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07167
47630739 = yrday
fracday
Element set: 910
Inclination: 51
6317 deg
RA of node: 107
5686 deg
Eccentricity:
0008513
Arg of perigee: 326
1323 deg
Mean anomaly: 33
9298 deg
Mean motion: 15
78454183 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1066
Checksum: 300
Coasting Arc #12 (Orbit 1081)
---------------------------------------
Vector Time (GMT): 2007/168/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1666586
76 A = 6719362
25 meter
Y = -6496455
25 meter E =
0003523
Z = -400860
24 I = 51
96635
XDOT = 4515
960094 Wp = 108
33026
YDOT = 1529
087727 meter/sec RA = 101
70851 deg
ZDOT = -6049
736495 TA = 76
01393
MA = 75
97476
Ha = 183
975 n
mi
Hp = 177
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5467804
34 X = 1741054
50
Y = -21313829
57 feet Y = -6477402
09 meter
Z = -1315158
26 Z = -392584
57
XDOT = 14816
142040 XDOT = 4527
914191
YDOT = 5016
692017 feet/sec YDOT = 1579
655875 meter/sec
ZDOT = -19848
216847 ZDOT = -6027
768816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18065695
29 X = -5506423
93
Y = -12565280
56 feet Y = -3829897
52 meter
Z = -1284614
45 Z = -391550
49
XDOT = 8991
784951 XDOT = 2740
696053
YDOT = -10922
384022 feet/sec YDOT = -3329
142650 meter/sec
ZDOT = -19765
012490 ZDOT = -6024
375807
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 07168
48925766
00020000 00000-0 20000-3 0 9110
2 25544 51
6325 102
3315 0008570 329
9800 30
0873 15
78489152 10822
Satellite: ISS
Catalog Number: 25544
Epoch time: 07168
48925766 = yrday
fracday
Element set: 911
Inclination: 51
6325 deg
RA of node: 102
3315 deg
Eccentricity:
0008570
Arg of perigee: 329
9800 deg
Mean anomaly: 30
0873 deg
Mean motion: 15
78489152 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1082
Checksum: 294
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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